
Carla Mattix
Examiner (ID: 2572)
| Most Active Art Unit | 3106 |
| Art Unit(s) | 3106, 3105 |
| Total Applications | 310 |
| Issued Applications | 284 |
| Pending Applications | 4 |
| Abandoned Applications | 22 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 2680762
[patent_doc_number] => 05064145
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-11-12
[patent_title] => 'Model airplane with tail assembly'
[patent_app_type] => 1
[patent_app_number] => 7/585663
[patent_app_country] => US
[patent_app_date] => 1990-09-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1708
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 188
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/064/05064145.pdf
[firstpage_image] =>[orig_patent_app_number] => 585663
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/585663 | Model airplane with tail assembly | Sep 19, 1990 | Issued |
Array
(
[id] => 2821814
[patent_doc_number] => 05120005
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-06-09
[patent_title] => 'Exhaust flap speedbrake'
[patent_app_type] => 1
[patent_app_number] => 7/582319
[patent_app_country] => US
[patent_app_date] => 1990-09-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 3022
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 158
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/120/05120005.pdf
[firstpage_image] =>[orig_patent_app_number] => 582319
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/582319 | Exhaust flap speedbrake | Sep 13, 1990 | Issued |
Array
(
[id] => 2721270
[patent_doc_number] => 05039036
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-08-13
[patent_title] => 'Energy absorbing air drop pallet'
[patent_app_type] => 1
[patent_app_number] => 7/580690
[patent_app_country] => US
[patent_app_date] => 1990-09-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 1453
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 182
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/039/05039036.pdf
[firstpage_image] =>[orig_patent_app_number] => 580690
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/580690 | Energy absorbing air drop pallet | Sep 10, 1990 | Issued |
Array
(
[id] => 2852881
[patent_doc_number] => 05096140
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-03-17
[patent_title] => 'Aircraft with engine pods tiltable about a transverse axis'
[patent_app_type] => 1
[patent_app_number] => 7/578037
[patent_app_country] => US
[patent_app_date] => 1990-09-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 11
[patent_no_of_words] => 4453
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 30
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/096/05096140.pdf
[firstpage_image] =>[orig_patent_app_number] => 578037
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/578037 | Aircraft with engine pods tiltable about a transverse axis | Sep 4, 1990 | Issued |
Array
(
[id] => 2783090
[patent_doc_number] => 05143327
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-09-01
[patent_title] => 'Integrated launch and emergency vehicle system'
[patent_app_type] => 1
[patent_app_number] => 7/575737
[patent_app_country] => US
[patent_app_date] => 1990-08-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 9
[patent_no_of_words] => 2477
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 162
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/143/05143327.pdf
[firstpage_image] =>[orig_patent_app_number] => 575737
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/575737 | Integrated launch and emergency vehicle system | Aug 30, 1990 | Issued |
Array
(
[id] => 2789383
[patent_doc_number] => 05114103
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-05-19
[patent_title] => 'Aircraft engine electrically powered boundary layer bleed system'
[patent_app_type] => 1
[patent_app_number] => 7/572825
[patent_app_country] => US
[patent_app_date] => 1990-08-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3797
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 167
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/114/05114103.pdf
[firstpage_image] =>[orig_patent_app_number] => 572825
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/572825 | Aircraft engine electrically powered boundary layer bleed system | Aug 26, 1990 | Issued |
Array
(
[id] => 2733745
[patent_doc_number] => 05037043
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-08-06
[patent_title] => 'Locking arrangement for unfolded solar generators'
[patent_app_type] => 1
[patent_app_number] => 7/571412
[patent_app_country] => US
[patent_app_date] => 1990-08-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 3318
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 313
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/037/05037043.pdf
[firstpage_image] =>[orig_patent_app_number] => 571412
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/571412 | Locking arrangement for unfolded solar generators | Aug 22, 1990 | Issued |
Array
(
[id] => 2722359
[patent_doc_number] => 05050819
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-09-24
[patent_title] => 'Rotatable non-circular forebody flow controller'
[patent_app_type] => 1
[patent_app_number] => 7/565090
[patent_app_country] => US
[patent_app_date] => 1990-08-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 16
[patent_no_of_words] => 2210
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 81
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/050/05050819.pdf
[firstpage_image] =>[orig_patent_app_number] => 565090
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/565090 | Rotatable non-circular forebody flow controller | Aug 9, 1990 | Issued |
Array
(
[id] => 2849157
[patent_doc_number] => 05082205
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-01-21
[patent_title] => 'Semi-buoyant composite aircraft with non-rotating aerostat'
[patent_app_type] => 1
[patent_app_number] => 7/564645
[patent_app_country] => US
[patent_app_date] => 1990-08-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 15
[patent_no_of_words] => 1486
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 192
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/082/05082205.pdf
[firstpage_image] =>[orig_patent_app_number] => 564645
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/564645 | Semi-buoyant composite aircraft with non-rotating aerostat | Aug 8, 1990 | Issued |
Array
(
[id] => 2811911
[patent_doc_number] => 05172876
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-12-22
[patent_title] => 'Spin reorientation maneuver for spinning spacecraft'
[patent_app_type] => 1
[patent_app_number] => 7/563161
[patent_app_country] => US
[patent_app_date] => 1990-08-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 17
[patent_no_of_words] => 4858
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 8
[patent_words_short_claim] => 109
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/172/05172876.pdf
[firstpage_image] =>[orig_patent_app_number] => 563161
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/563161 | Spin reorientation maneuver for spinning spacecraft | Aug 2, 1990 | Issued |
Array
(
[id] => 2720959
[patent_doc_number] => 05076514
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-12-31
[patent_title] => 'Apparatus for latching two parts together'
[patent_app_type] => 1
[patent_app_number] => 7/562170
[patent_app_country] => US
[patent_app_date] => 1990-08-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 11
[patent_no_of_words] => 2201
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 241
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/076/05076514.pdf
[firstpage_image] =>[orig_patent_app_number] => 562170
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/562170 | Apparatus for latching two parts together | Aug 2, 1990 | Issued |
Array
(
[id] => 2852948
[patent_doc_number] => 05096143
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-03-17
[patent_title] => 'Tail unit with rotatable tailplane'
[patent_app_type] => 1
[patent_app_number] => 7/559949
[patent_app_country] => US
[patent_app_date] => 1990-07-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 1379
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 125
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/096/05096143.pdf
[firstpage_image] =>[orig_patent_app_number] => 559949
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/559949 | Tail unit with rotatable tailplane | Jul 30, 1990 | Issued |
Array
(
[id] => 2744095
[patent_doc_number] => 05058828
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-10-22
[patent_title] => 'Overwing thrust reverser'
[patent_app_type] => 1
[patent_app_number] => 7/559815
[patent_app_country] => US
[patent_app_date] => 1990-07-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 4375
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 397
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/058/05058828.pdf
[firstpage_image] =>[orig_patent_app_number] => 559815
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/559815 | Overwing thrust reverser | Jul 29, 1990 | Issued |
Array
(
[id] => 2809495
[patent_doc_number] => 05167383
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-12-01
[patent_title] => 'STOL aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/557809
[patent_app_country] => US
[patent_app_date] => 1990-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 13
[patent_no_of_words] => 4500
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 189
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/167/05167383.pdf
[firstpage_image] =>[orig_patent_app_number] => 557809
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/557809 | STOL aircraft | Jul 25, 1990 | Issued |
Array
(
[id] => 2731551
[patent_doc_number] => 05036924
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-08-06
[patent_title] => 'Container fire nozzle hole adapter'
[patent_app_type] => 1
[patent_app_number] => 7/557466
[patent_app_country] => US
[patent_app_date] => 1990-07-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 8
[patent_no_of_words] => 1105
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 270
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/036/05036924.pdf
[firstpage_image] =>[orig_patent_app_number] => 557466
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/557466 | Container fire nozzle hole adapter | Jul 24, 1990 | Issued |
Array
(
[id] => 2737819
[patent_doc_number] => 05071089
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-12-10
[patent_title] => 'Off weight lift wing for skiers and the like'
[patent_app_type] => 1
[patent_app_number] => 7/557660
[patent_app_country] => US
[patent_app_date] => 1990-07-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 4
[patent_no_of_words] => 923
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 159
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/071/05071089.pdf
[firstpage_image] =>[orig_patent_app_number] => 557660
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/557660 | Off weight lift wing for skiers and the like | Jul 24, 1990 | Issued |
Array
(
[id] => 2770124
[patent_doc_number] => 05086996
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-02-11
[patent_title] => 'High-capacity fuselage for aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/549970
[patent_app_country] => US
[patent_app_date] => 1990-07-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 36
[patent_no_of_words] => 8689
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 208
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/086/05086996.pdf
[firstpage_image] =>[orig_patent_app_number] => 549970
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/549970 | High-capacity fuselage for aircraft | Jul 8, 1990 | Issued |
Array
(
[id] => 2849131
[patent_doc_number] => 05082204
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-01-21
[patent_title] => 'All wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/546550
[patent_app_country] => US
[patent_app_date] => 1990-06-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 9
[patent_no_of_words] => 10466
[patent_no_of_claims] => 30
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/082/05082204.pdf
[firstpage_image] =>[orig_patent_app_number] => 546550
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/546550 | All wing aircraft | Jun 28, 1990 | Issued |
Array
(
[id] => 2810151
[patent_doc_number] => 05115998
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-05-26
[patent_title] => 'Annular balloon'
[patent_app_type] => 1
[patent_app_number] => 7/546134
[patent_app_country] => US
[patent_app_date] => 1990-06-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 1703
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/115/05115998.pdf
[firstpage_image] =>[orig_patent_app_number] => 546134
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/546134 | Annular balloon | Jun 28, 1990 | Issued |
Array
(
[id] => 2769590
[patent_doc_number] => 05141180
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-08-25
[patent_title] => 'Satellite attitude control system using a superconducting magnetic loop'
[patent_app_type] => 1
[patent_app_number] => 7/542140
[patent_app_country] => US
[patent_app_date] => 1990-06-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 3026
[patent_no_of_claims] => 10
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[patent_words_short_claim] => 133
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/141/05141180.pdf
[firstpage_image] =>[orig_patent_app_number] => 542140
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/542140 | Satellite attitude control system using a superconducting magnetic loop | Jun 21, 1990 | Issued |